JASC 5321
Service difficulty reports · 49,350
Reports filed under 5321 · Fuselage Floor Panel, newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5321' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5321' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWAA2023091289427Floor Panel · brokenFWD FLOOR PANEL 221GF FWD O/B TANG IS BROKEN.<[01] REPAIRED FWD FLOOR PANEL 221GF FWD O/B TANG IAW SRM 53-00-50-2R-6.<BR><BR>ATTACHED CURE SHEETS TO FAULT.;[02] VERIFIED CORRECTIVE ACTION ITEMS AND MEASUREMENT FIELDS; CARD COMPLETE.SDR SWAA2023091189428Floor Panel · pulledFWD FLOOR PANEL 221GF UPPER SKIN HAS AREAS OF PULLED STRANDS<[01] REPAIRED FWD FLOOR PANEL 221GF UPPER SKIN IAW SRM 53-00-50-2R-1 AND BOEING DWG 141A5810<BR><BR>ATTACHED CURE SHEETS TO FAULT.;[02] VERIFIED CORRECTIVE ACTION ITEMS AND MEASUREMENT FIELDS; CARD CSDR SWAA2023091189429Floor Panel · pulledFWD FLOOR PANEL 222AF UPPER SKIN HAS AREA OF PULLED STRANDS<[01] REPAIRED UPPER SURFACE SKIN ON FWD FLOOR PANEL 222AF IAW SRM 53-00-50-2R-1 AND BOEING DWG 141A7810.<BR><BR>ATTACHED CURE SHEETS TO FAULT.;[02] VERIFIED CORRECTIVE ACTION ITEM AND MEASUREMENT FIELSDR SWAA2023091189421Floor Panel · pulledFLOOR PANEL 242PF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF ALL THE DAMAGE; DECIDED TO FABRICATE A NEW FLOOR PANEL WITH BMS4-23 TYPE II LOT 1531001-1 AND BMS5-107 LOT AK2KP8383K-1 RESIN; CURED THE RESIN; UNDER A HEAT LAMP; USING THERMOMSDR SWAA2023091189422Floor Panel · delaminatedFLOOR PANEL 242QF FWD O/B CORNER IS DELAMINATED.<[01] DELAMINATED BOARD WAS REPLACED WITH BOARD FABRICATED FROM RAW STOCK IAW SRM 53-00-50-2R-0 AND DRAWING 146A5810 SHEET 468.<BR><BR>UPLOADED CURE SHEET.<BR><BR>JOB COMPLETE.;[02] VERIFIED JOB COMPLETE; VERIFIESDR SWAA2023091189430Floor Panel · pulledAFT FLOOR PANEL 241XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] IDENTIFIED THE PANEL IAW SRM 53-00-50-0I-1 FIGURE 6 AND TABLE 6. THE DAMAGE TO THE PANEL IS BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F AND WILL BE REPAIRED IAW SRM 53-00-50-2R-SDR SWAA2023091189431Floor Panel · pulledAFT FLOOR PANEL 241YF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241YF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[02] VERIFIED CORRECTIVE ACTION 1.SDR SWAA2023091189432Floor Panel · pulledAFT FLOOR PANEL 241ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ZF UPPER SKIN WITH AREAS OF PULLED STRAND WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[02] VERIFIED CORRECTIVE ACTION #1<BR>VERIFIED MEASURSDR SWAA2023091189433Floor Panel · pulledAFT FLOOR PANEL 241AAF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241AAF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATE FLOOR PANEL PER SRM 53-00-50-2R-0. ATTACHED CURE SHEET TO THIS FAULT RECORD.;[02] VERIFIED COSDR SWAA2023091189423Floor Panel · pulledAFT FLOOR PANEL 241ADF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ADF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[02] VERIFIED CORRECTIVE ACTION #1;[03] VERIFIED MSDR SWAA2023091189436Floor Panel · pulledAFT FLOOR PANEL 242TF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] REPAIRED AREAS OF PULLED STRANDS ON UPPER SKIN OF AFT FLOOR PANEL 242TF IAW SRM 53-00-50-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.;[03] VERIFIED MEASUREMENTS TABLE.SDR SWAA2023091189437Floor Panel · pulledAFT FLOOR PANEL 242UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242UF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE RECORDS TO THIS FAULT.;[02] VERIFIED RII STEPS COMPLETE;[03] VERIFIED MEASUREMENTSDR SWAA2023090689882Floor Panel · pulledFWD FLOOR PANEL 222DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AREA OF PULLED STRANDS ON UPPER SKIN OF FWD FLOOR PANEL 222DF WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED RII STEPS COMPLETE;[03] VERIFIED JOB COMPLETE AND MEASUREMENT TABLESDR SWAA2023090689880Floor Panel · pulledFWD FLOOR PANEL 221FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] I UPDATED THE MEASUREMENTS TABLE.;[02] FWD FLOOR PANEL 221FF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[03] VERIFIEDSDR SWAA2023090689879Floor Panel · pulledFWD FLOOR PANEL 221EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221EF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED RII STEPS COMPLETE;[03] VERIFIED JOB COMPLETESDR SWAA2023090689883Floor Panel · pulledFWD FLOOR PANEL 221CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] UPDATED THE MEASUREMENT TABLE.;[02] FWD FLOOR PANEL 221CF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[03] VERIFIED RISDR SWAA2023090689373Floor Panel · pulledAFT FLOOR PANEL 242VF UPPER SKIN HAS PULLED STRANDS<[01] PULLED STRANDS ON UPPER SURFACE SKIN OF AFT PANEL 242VF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED JOB COMPLETE AND CURE SHEETS;[03] EDITED STEPS TO INCLUDE RII INSPECTION ITEMS.;[04] FINAL INSPESDR SWAA2023090689369Floor Panel · pulledAFT FLOOR PANEL 241ACF UPPER SKIN HAS PULLED STRANDS<[01] FLOOR PANEL 241ACF UPPER SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>ATTACHED ALL CURE SHEETS TO THIS FAULT.;[02] FINAL INSPECTION. JOB COMPLETE.;[03] FINAL INSPECTION. JOB COMPLETE.SDR SWAA2023090689367Floor Panel · pulledAFT FLOOR PANEL 241AAF UPPER SKIN HAS PULLED STRANDS<[01] FABRICATED REPLACEMENT FLOOR PANEL 241AAF IAW SRM 53-00-50-2R-0 AND BOEING DWG: 147A5810 ID: 0008.;[02] FINAL INSPECTION. JOB COMPLETE.SDR SWAA2023090689366Floor Panel · pulledAFT FLOOR PANEL 241ZF UPPER SKIN HAS PULLED STRANDS.<[01] PULLED STRANDS ON UPPER SURFACE SKIN OF AFT PANEL 241ZF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED RII STEPS COMPLETE;[03] VERIFIED JOB COMPLETE AND MEASUREMENT TABLESDR SWAA2023090689363Floor Panel · damagedFLOOR PANEL 232SF IS MISSING AN INSERT ALONG THE O/B EDGE. (MARKED)<[01] FOUND DAMAGE AT MISSING INSERT LOCATION ON O/B EDGE OF FLOOR PANEL 232SF; DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 232SF FROM BMS 4-23TY2 LOT#1534174-1; INSTALLED INSERTS USDR AALA202308169459Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 231LF DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.SDR SWAA2023081689216Floor Panel · separatedAFT CARGO LH SIDE; SECOND PANEL AFT OF BULKHEAD SEPERATED FROM FLOOR<[01] OK TO CONTINUE PER MEL 25-16-01; SP1B;[02] R&R CARGO PANELS 141DW & 141FW IAW AMM 25-52-06SDR SWAA2023081690187Floor Panel · separatedAFT CARGO LH SIDE; SECOND PANEL AFT OF BULKHEAD SEPERATED FROM FLOOR<[01] OK TO CONTINUE PER MEL 25-16-01; SP1B;[02] R&R CARGO PANELS 141DW & 141FW IAW AMM 25-52-06SDR SWAA2023092188748Floor Panel · delaminatedCABIN FLOOR PANEL# 241AF DELAMINATED.<[01] FABRICATED FLOOR PANEL 241AF REF: DWG# 144A5810-127 AND SRM 53-00-50-2R-0 INSTALLATION WILL BE ACCOMPLISH ON CLOSING CARD : TTG8Q00MDT9J;[02] VERIFIED AND INSPECTED STEP #1; FABRICATED FLOOR PANEL 241AF.SDR SWAA2023092188747Floor Panel · delaminatedCABIN FLOOR PANEL #231XF DELAMINATED.<[01] RECIEVED NEW FLOOR PANEL PART #144A5810-126; CLOSING WILL BE ACCOMPLISHED ON FAULT TTG8Q00MDTCE.;[02] VERIFIEDSDR SWAA2023092188753Floor Panel · delaminatedCABIN FLOOR PANEL# 241DF DELAMINATED.<[01] RECIEVED NEW FLOOR PANEL PART #144A5810-128; CLOSING WILL BE ACCOMPLISHED ON FAULT TTG8Q00MDT9C.;[02] VERIFIEDSDR SWAA2023092188751Floor Panel · delaminatedCABIN FLOOR PANEL #232SF DELAMINATED.<[01] RECIEVED NEW FLOOR PANEL PART #144A5810-161; CLOSING WILL BE ACCOMPLISHED ON FAULT TTG8Q00MDTBC.;[02] VERIFIEDSDR ASAA2023081144715Floor Panel · delaminatedOVER WING FLOOR PANEL P/N 144A5810-126 CENTER AISLE (PANEL #231XF) HAS SKIN DELAM. GROUNDED - YES. REPAIRED OVERWING FLOOR PANEL P/N:144A5810-126 CENTER AISLE (PANEL# 231XF)SKIN DELAM IAW B737-900 SRM 53-00-50.SDR ASAA2023081144714Floor Panel · delaminatedOVER WING FLOOR PANEL P/N 144A5810-124 R/H SIDE (PANEL #232RF) HAS SKINDELAM. GROUNDED - YES. CLEANED SANDED & REMOVED DAMAGE ON OVERWING FLOOR PANEL P/N 144A5810-124 R/H SIDE (PANEL #232RF) AND REPAIRED IAW B737SRM 53-00-50-2R-1.SDR ASAA2023081144713Floor Panel · delaminatedOVER WING FLOOR PANEL P/N 144A5810-189 R/H SIDE (PANEL #242AF) HAS SKIN DELAM. GROUNDED - YES. CLEANED, SANDED & REMOVED DAMAGE ON OVERWING FLOOR PANEL P/N 144A5810-189 R/H SIDE (PANEL #242AF) AND REPAIRED IAW B737SRM 53-00-50-2R-1.SDR ASAA2023081144711Floor Panel · delaminatedOVER WING FLOOR PANEL P/N 144A5810-124 L/H SIDE (PANEL #231YF) HAS SKIN DELAM. GROUNDED - YES. REPAIRED OVER WING FLOOR PANEL P/N: 144A5810-124 L/H SIDE (PANEL #231YF) SKIN DELAM IAW B737-900 SRM 53-00-50.SDR SWAA2023082487783Floor Panel · delaminatedFLOOR PANEL 241SF UPPER SURFACE IS DELAMINATED.<[01] IDENTIFIED FLOOR PANEL 241SF IAW SRM 53-00-50-0I-1 FIG 5 TABLE 5 AND BOEING DWG 146A5810 ID:0102.<BR><BR>FOUND DELAMINATION DAMAGE TO UPPER SURFACE SKIN PLIES TO BE OUT OFF ALLOWABLE DAMAGE LIMITS IAW SRM 53SDR SWAA2023082487777Floor Panel · delaminatedFLOOR PANEL 241RF UPPER SURFACE IS DELAMINATED.<[01] IDENTIFIED FLOOR PANEL 241RF MATERIALS IAW SRM 53-00-50-0I-1 FIG 5 TABLE 5 AND BOEING DWG 146A5810 ID:0011.<BR><BR>FOUND DELAMINATION DAMAGE TO UPPER SURFACE SKIN PLIES TO BE OUT OF ALLOWABLE DAMAGE LIMITS ISDR DALA2023081106576Unknown · unknownSHIP 3144 AD RELATED INSIDE 510 TROLLEY AREA COMPARTMENT FOUND CRACK AND MEASURE .300. CORRECTIVE ACTION: REPLACED 510 TROLLEY AREA COMPARTMENT PER AD 2022-24-05. (2911378)SDR FDEA202308101393Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241MF(P/N:152W8402-17) AT STA1290/LBL105.5-107.5 FOUND CRACK(OFF WING). EVALUATED MAIN DECK CARGO FLOOR PANEL 241MF(P/N:152W8402-17) CRACK, THE DAMAGE SIZE : L=2.2", OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DSDR FDEA202308101392Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242KF(P/N:152W8402-18) AT STA1269.5/RBL81-83.25 FOUND CRACK(OFF WING). EVALUATED MAIN DECK CARGO FLOOR PANEL 242KF(P/N:152W8402-18) CRACK ,THE DAMAGE SIZE :L=2.3" , OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DSDR SWAA2023092187862Floor Panel · corrodedCORROSION ON AFT WET AREA FLOOR PANEL 241D INSERTS NEAR AFT MOUNT FITTINGS.<[01] REPLACED CABIN FLOOR PANEL 241D AS PER SRM 53-00-50-1A-1.;[02] VERIFIED REPLACEDSDR SWAA2023092187864Floor Panel · corrodedCORROSION ON AFT CABIN WET AREA FLOOR PANEL 242D INSERT AT AFT O/B CORNER.<[01] REPLACED AFT CABIN WET AREA FLOOR PANEL 242D IN REFERENCE TO SRM 53-00-50-1A-1.;[02] VERIFIED REPLACEMENTSDR SWAA2023092187531Floor Panel · crackedFORWARD CABIN WET AREA FLOOR PANEL 222BF IS CRACKED AND INSERT PULLED THROUGH AT THE O/B AFT CORNER.<[01] RECEIVED NEW FLOOR PANEL (222BF) P/N 141A5810-464; VERIFIED APPLICABILITY PER 737-800 AIPC 53-21-51-22B;[02] VERIFIED RECEIVEDSDR SWAA2023092187536Floor Panel · peelingAFT WET AREA CABIN FLOOR PANEL 241F UPPER LAMINATE PEELING.<[01] REPLACED AFT WET AREA CABIN FLOOR PANEL 241F AS PER SRM 53-00-50-1A-1.;[02] VERIFIED REPLACEMENTSDR SWAA2023092187537Floor Panel · pulledAFT WET AREA CABIN FLOOR PANEL 242E INSERT PULLED THROUGH AT O/B AFT CORNER.<[01] REPLACED CABIN FLOOR PANEL 242E AS PER SRM 53-00-50-1A-1.;[02] VERIFIED REPLACEMENTSDR SWAA2023092187859Floor Panel · peelingAFT WET AREA CABIN FLOOR PANEL 241ABF UPPER LAMINATE PEELING.<[01] REPLACED AFT WET AREA CABIN FLOOR PANEL 241ABF AS PER SRM 53-00-50-1A-1.;[02] VERIFIED REPLACEMENTSDR SWAA2023092187863Floor Panel · pulledAFT WET AREA CABIN FLOOR PANEL 241E INSERT PULLED THROUGH AT AFT O/B CORNER.<[01] REPLACED CABIN FLOOR PANEL 241E AS PER SRM 53-00-50-1A-1.;[02] VERIFIED REPLACEMENTSDR SWAA2023092187865Floor Panel · peelingAFT WET AREA CABIN FLOOR PANEL 241XF LAMINATE PEELING ON UPPER SURFACE.<[01] REPLACED CABIN FLOOR PANEL 241XF AS PER SRM 53-00-50-1A-1.;[02] VERIFIED REPLACEMENTSDR AALA202308114884Floor Panel · damagedAIRCRAFT WAS GROUNDED: AISLE CABIN FLOOR PANEL BETWEEN SEAT ROWS 1 AND 2 VERY SOFT AND BOUNCY. MAINTENANCE REPAIRED FLOOR PANEL PER AARD 53-00-00-6.SDR IPXA2023081493909Floor Panel · damagedINSPECTION TYPE:C*** MAJOR REPAIR *** PNL 131BH IS DAMAGED.FABBED PNL 131BH PER SREO A300-5320-16407.SDR IPXA2023081493910Floor Panel · damagedINSPECTION TYPE:C*** MAJOR REPAIR *** PNL 131GE IS DAMAGED.FABBED PNL 131GE PER SREO A300-5320-16407.SDR IPXA2023081493908Floor Panel · damagedINSPECTION TYPE:C*** MAJOR REPAIR *** PNL 131MG IS DAMAGED.FABBED PNL 131MG PER SREO A300-5320-16407.SDR IPXA2023081493907Floor Panel · damagedINSPECTION TYPE:C*** MAJOR REPAIR *** PNL 131AH IS DAMAGED.FABBED PNL 131AH PER SREO A300-5320-16407.
Back to JASC 5321